Assessment of Installed Turbofan Performance & Stability of Advanced Aircraft
Advisors: Professor Spakovszky, Professor Greitzer
How do we define the prosulsion system for high subsonic aircrafts antecipating and eliminating risks related to the propulsion airframe integration? This research aims to anwser this question through a modeling framework capable of assessing fan performance and stability with inlet distortion and inlet-fan coupling. The goal is to provide installed turbofan design guidelines to mitigate the risks associated with the integration of propulsion system on novel aircrafts configurations. .
